McDonnell Douglas F-4 Phantom II vs. Beechcraft T-6 Texan II

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McDonnell Douglas F-4 Phantom II versus Beechcraft T-6 Texan II
19.2 m 63 ft 0 in length 10.18 m 33 ft 4 in
5.03 m 16 ft 6 in height 3.29 m 10 ft 10 in
11.72 m 38 ft 5 in wingspan 10.21 m 33 ft 6 in
Two General Electric J79s engines 1 x Pratt & Whitney Canada PT6A-68
17,900 lbs thrust per engine 1100 lbs
35,800 lbs total thrust 1100 lbs
27,965 kg 61,700 lb MTOW 6,250 lb 2,835 kg
3,031 km 1,636 nm range 900 nm 1,667 km
Mach 2.2 2,717 km/h cruise speed 320 kts 199 mph
Up to 16,000 lbs of externally carried ordnance capacity 2
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.